Fixed typos

Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s

@@ -82,7 +82,7 @@
 #	IN R2 THE BBCON OF SELF-CHECK, AND IN R3 THE TOTAL NUMBER OF ERRORS DETECTED BY SELF-CHECK SINCE THE LAST MAN
 #	INITIATED FRESH START (SLAP1).
 #
-#	SHOW-BANKSUM STARTING WTIH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
+#	SHOW-BANKSUM STARTING WITH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
 #	THE BANK NUMBER, AND IN R3 THE BUGGER WORD.
 #
 # ERASABLE INITIALIZATION REQUIRED

Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s

@@ -250,7 +250,7 @@
 
 # Page 8
 # IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
-# CONTAINS AT LEAST ONE COMONENT WHICH CANNOT BE LOADED, I.E. OF
+# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
 # SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS).
 
 # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
@@ -1033,7 +1033,7 @@
 # 00005		SPECIFY SOR PHASE		1=FIRST 2=SECOND		P38		COLOSSUS + LUMINARY
 # 00006		SPECIFY RR COARSE ALIGN OPTION	1=LOCKON 2=CONTINUOUS DESIG.	V41N72		SUNDANCE + LUMINARY
 # 00007		SPECIFY PROPULSION SYSTEM	1=SPS 2=RCS			P37		COLOSSUS
-# 00010		SPECIFY ALIGNEMENT MODE		0=ANY TIME 1=REFSMMAT + G	P57		LUMINARY	
+# 00010		SPECIFY ALIGNMENT MODE		0=ANY TIME 1=REFSMMAT + G	P57		LUMINARY	
 #						2=TWO BODIES 3=ONE BODY + G
 # 00011		SPEC. SEPARATION MONITOR PHASE	1=DELTAV 2=STATE VECTOR UPDATE	P46		LUMINARY
 # 00012		SPECIFY CSM ORBIT OPTION	1=NO ORBIT CHANGE 2=CHANGE	P22		LUMINARY

Comanche055/AUTOMATIC_MANEUVERS.s

@@ -490,7 +490,7 @@ ZEROCMDS	CAF	ZERO
 		TS	TAU1
 		TS	TAU2
 T6PROG		EXTEND			# WHEN THE ROTATION COMMANDS (TAUS)
-		DCA	JETADDR		# HAVE BEEN DETERINED
+		DCA	JETADDR		# HAVE BEEN DETERMINED
 		DXCH	T5LOC		# RESET T5LOC FOR PHASE3
 		TCF	RESUME
 		

Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s

@@ -32,7 +32,7 @@
 
 # Page 1063
 # SUBROUTINE TO READ GIMBAL ANGLES AND FORM DIFFERENCES.  GIMBAL ANGLES ARE SAVED IN 2'S COMPLEMENT, BUT THE
-# DIFFERENECES ARE IN 1'S COMP.  ENTER AND READ ANGLES EACH .1 SEC.
+# DIFFERENCES ARE IN 1'S COMP.  ENTER AND READ ANGLES EACH .1 SEC.
 #
 #	CM/DSTBY = 1 FOR DAP OPERATION
 #	CM/DSTBY = 0 TO TERMINATE DAP OPERATION
@@ -289,7 +289,7 @@ T5IDLER1	2CADR	T5IDLOC
 
 # Page 1070
 # THIS SECTION CALCULATES THE ANGULAR BODY RATES EACH .1 SEC.  THE ANGULAR RATES ARE THOSE ALONG THE BODY AXES
-# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R.	REQIREMENT:  TEMPORARILY ERASE.  JETEM, JETEM +1
+# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R.	REQUIREMENT:  TEMPORARILY ERASE.  JETEM, JETEM +1
 #
 # SINCE RESTARTS ZERO THE JET OUTPUT CHANNELS, NO ATTEMPT IS MADE TO RESTART THE ENTRY DAPS.  THAT IS,
 # THE 0.1 SEC DAPS WILL MISS A CYCLE, AND WILL PICK UP AT THE NEXT 0.1 SEC UPDATE.  MOST OF THE TIME THE 2 SEC
@@ -1079,7 +1079,7 @@ TIMETST5	CS	ONE
 		
 # SECTION  JETCALL  EXAMINES CONTENTS OF JET TIMES IN LIST, ESTABLISHES WTLST ENTRIES, AND EXECUTES CORRESPONDING
 # JET CODES.  A POSITIVE NZ NUMBER IN A TIME REGISTER INDICATES THAT A WTLST CALL IS TO BE MADE, AND ITS JET BITS
-# EXECUTED.  A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPOINDING JET BITS ARE TO BE
+# EXECUTED.  A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPONDING JET BITS ARE TO BE
 # EXECUTED.  A NEG NUMBER INDICATES THAT THE TIME INTERVAL HAS BEEN PROCESSED.  IN EVENT OF +0 OR -1, THE 
 # SUBSEQUENT TIME REGISTER IS EXAMINED FOR POSSIBLE ACTION.  THUS JET BITS TO BE EXECUTED MAY COME FROM MORE
 # THAN ONE REGISTER.

Comanche055/CONIC_SUBROUTINES.s

@@ -106,7 +106,7 @@
 #							RESPECTIVELY, IS THE CENTRAL BODY
 #	TAU		+28			DESIRED TRANSFER TIME IN CENTISECONDS (DP)
 #							MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
-#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WTIH THAT OF TAU.
+#	XKEPNEW		+17 FOR EARTH		DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU.
 #			+16 FOR MOON			AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
 #							MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
 #							BY KEPLER TO A POOR BUT VALID GUESS.
@@ -286,7 +286,7 @@
 #	STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
 #	PROVIDES THE OPTION OF COMUTING THE NEW UPDATED STATE VECTOR.  THE RESULTING TRAJECTORY MAY BE A SECTION OF A
 #	CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON.  THE USE OF THE SUBROUTINE CAN BE
-# 	EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WTIHOUT INTRODUCING ANY CODING CHANGES,
+# 	EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
 #	ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
 #
 # THE RESTRICTIONS ARE --
@@ -1776,7 +1776,7 @@ MUTABLE		2DEC*	3.986032 E10 B-36*	# MUE
 
 LDPOSMAX	EQUALS 	LODPMAX			# DPPOSMAX IN LOW MEMORY.
 
-# ERASABLE ASSIGNEMENTS
+# ERASABLE ASSIGNMENTS
 
 # KEPLER SUBROUTINE
 

Comanche055/CSM_GEOMETRY.s

@@ -33,7 +33,7 @@
 		BANK
 		
 # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
-# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT.
+# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
 #
 # THE INPUTS ARE:  1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
 # MARK VAC AREA.  2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR

Comanche055/DISPLAY_INTERFACE_ROUTINES.s

@@ -485,7 +485,7 @@
 #	5.  IT IS ALWAYS GOOD PRACTICE TO TERMINATE AN EXTENDED VERB BEFORE ASKING FOR ANOTHER ONE OR THE SAME ONE
 #	    OVER AGAIN.
 #
-# SPECIAL CONSIDERATONS --
+# SPECIAL CONSIDERATIONS --
 # Page 1464
 #	1.  MPAC +2 SAVED ONLY IN MARK DISPLAYS
 #	2.  GODSP(R), REGODSP(R), GOMARK(R) ALWAYS TURN ON THE FLASH IF ENTERED WITH A PASTE VERB REQUEST.
@@ -638,7 +638,7 @@ COPYPACS	INDEX	COPINDEX
 
 		TC	Q
 
-# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERUPTING A GOPLAY DISPLAY
+# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERRUPTING A GOPLAY DISPLAY
 # (A NORMAL OR A PRIO).  IF THE ASTRONAUT TRIES TO MARK DURING A PRIO, THE CHECK FAIL LIGHT GOES ON AND THE MARK
 # REQUEST IS ENDED.  IF HE TRIES TO MARK DURING A NORM, THE MARK IS ALLOWED.  IN THIS CASE THE NORM IS PUT TO SLEEP
 # UNTIL ALL MARKING IS FINISHED.

Comanche055/DOWN-TELEMETRY_PROGRAM.s

@@ -106,7 +106,7 @@
 # 1.	DOWNLISTS.  DOWNLISTS MUST BE COMPILED IN THE SAME BANK AS THE
 #	DOWN-TELEMETRY PROGRAM.  THIS IS DONE FOR EASE OF CODING, FASTER
 #	EXECUTION.
-# 2.	EACH DOWNLINK LIST CONSISTES OF A CONTROL LIST AND A NUMBER OF
+# 2.	EACH DOWNLINK LIST CONSISTS OF A CONTROL LIST AND A NUMBER OF
 #	SUBLISTS.
 # 3.	A SUBLIST REFERS TO A SNAPSHOT OR DATA COMMON TO THE SAME OR OTHER
 #	DOWNLINK LISTS.  ANY SUBLIST CONTAINING COMMON DATA NEEDS TO BE
@@ -122,7 +122,7 @@
 #		SAME AS ECADR, BUT USED WHEN THE WORD ADDRESSED IS THE LEFT
 #		HALF OF A DOUBLE-PRECISION WORD FOR DOWN TELEMETRY.
 #	B.	2DNADR - 6DNADR		N-WORD DOWNLIST ADDRESS, N = 2 - 6.
-#		SAME AS 1DNADR, BUT WTIH THE 4 UNUSED BITS OF THE ECADR FORMAT
+#		SAME AS 1DNADR, BUT WITH THE 4 UNUSED BITS OF THE ECADR FORMAT
 #		FILLED IN WITH 0001-0101.  USED TO POINT TO A LIST OF N DOUBLE-
 #		PRECISION WORDS, STORED CONSECUTIVELY, FOR DOWN TELEMETRY.
 #	C.	DNCHAN			DOWNLIST CHANNEL ADDRESS.
@@ -347,7 +347,7 @@ SUBLIST		EQUALS 	DNQ
 #	AFTER KEYING IN V74E THE CURRENT DOWNLIST WILL BE IMMEDIATELY TERMINATED AND THE DOWNLINK ERASABLE DUMP
 #	WILL BEGIN.
 #
-#	ONCE INITITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
+#	ONCE INITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
 #	BY THE FOLLOWING:
 #
 #	1.	A FRESH START

Comanche055/EXECUTIVE.s

@@ -47,7 +47,7 @@ NOVAC		INHINT
 		TS	EXECTEM1
 		TCF	NOVAC2		# ENTER EXECUTIVE BANK.
 
-# TO ENTER A JOB REQUEST REQUIREING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
+# TO ENTER A JOB REQUEST REQUIRING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
 
 FINDVAC		INHINT
 		TS	NEWPRIO
@@ -157,7 +157,7 @@ NOVAC2		CAF	ZERO		# NOVAC ENTERS HERE.  FIND A CORE SET.
 NOVAC3		TS	EXECTEM2
 		INDEX	LOCCTR
 		CCS	PRIORITY	# EACH PRIORITY REGISTER CONTAINS -0 IF
-		TCF	NEXTCORE	# THE CORESPONDING CORE SET IS AVAILABLE.
+		TCF	NEXTCORE	# THE CORRESPONDING CORE SET IS AVAILABLE.
 NO.CORES	DEC	6
 		TCF	NEXTCORE	# AN ACTIVE JOB HAS A POSITIVE PRIORITY
 					# BUT A DORMANT JOB'S PRIORITY IS NEGATIVE
@@ -319,7 +319,7 @@ JOBWAKE3	CAF	COREINC
 		ADS	LOCCTR
 		CCS	EXECTEM2
 		TCF	JOBWAKE4
-		CS	ONE		# EXIT IF SLEEPIG JOB NOT FOUND.
+		CS	ONE		# EXIT IF SLEEPING JOB NOT FOUND.
 		TS	LOCCTR
 		TCF	ENDFIND
 

Comanche055/FRESH_START_AND_RESTART.s

@@ -99,7 +99,7 @@
 #
 #	1.	INTIALIZE OUTBIT CHANNELS 11,12,13, AND 14
 #	2.	REPLACE ALL TASKS ON WAITLIST WITH ENDTASK
-#	3.	MAKE ALL EXECUTEVE REGISTERS AVAILABLE
+#	3.	MAKE ALL EXECUTIVE REGISTERS AVAILABLE
 #	4.	MAKE ALL VAC AREAS AVAILABLE
 #	5.	CLEAR DSKY REGISTERS
 #	6.	ZERO NUMEROUS SWITCHES
@@ -130,7 +130,7 @@
 #	B.	ALARMS
 #
 #		1107	PHASE TABLE ERROR
-#		1110	RESTART WTIH NO ACTIVE GROUPS
+#		1110	RESTART WITH NO ACTIVE GROUPS
 
 # Page 183
 		BANK	10

Comanche055/INTERPRETER.s

@@ -2626,7 +2626,7 @@ NORMTEST	CCS	CYL		# SEE IF ARGUMENT NOW NORMALIZED AT
 
 # Page 1187
 # TRIGONOMETRIC FUNCTION PACKAGE.
-#	THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAIALABLE AS INTERPRETIVE OPERATIONS:
+#	THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAILABLE AS INTERPRETIVE OPERATIONS:
 #	1.	SIN		COMPUTES (1/2)SINE(2 PI MPAC).
 #	2.	COS		COMPUTES (1/2)COSINE(2 PI MPAC).
 #	3.	ASIN		COMPUTES (1/2PI)ARCSINE(2 MPAC).

Comanche055/JET_SELECTION_LOGIC.s

@@ -365,7 +365,7 @@ NOACY		CA	RWORD1		# Y-TRANSLATION NOT ACCEPTED
 # FAILURES.  IF THERE ARE BD FAILURES, Z-TRANSLATION COMMANDS WILL BE IGNORED, IN WHICH CASE THE ASTRONAUT SHOULD
 # SWITCH TO AC ROLL.
 #
-# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIREABLE ROLL
+# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIRABLE ROLL
 # INTRODUCED BY THIS TRANSLATION WILL BE COMPENSATED BY THE TWO AC ROLL JETS ACTUATED BY THE AUTOPILOT LOGIC.
 #
 # 					   WORD MAKE UP....RTABLE
@@ -386,7 +386,7 @@ NOACY		CA	RWORD1		# Y-TRANSLATION NOT ACCEPTED
 # THIS WORD MAY THEN BE ADDED TO THE WORD SELECTED FROM THE YZ-TRANSLATION TABLE, WHICH HAS THE SAME TYPE OF
 # CODING AS ABOVE, AND THE NET ROLL DETERMINED BY SHIFTING THE RESULTANT WORD RIGHT 8 PLACES AND SUBTRACTING FOUR.
 #
-# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTEPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
+# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTERPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
 # (AS ABOVE) TO GIVE THE NET ROLL TORQUE.
 
 					# ROLL 		TRANS		QUADFAIL	BIAS

Comanche055/KALCMANU_STEERING.s

@@ -89,7 +89,7 @@ INCRDCDU	TS	KSPNDX
 		TCF	INCRDCDU	# LOOP FOR THREE AXES
 		
 		RELINT		
-# COMPARE PRESENT TIME WTIH TIME TO TERMINATE MANEUVER
+# COMPARE PRESENT TIME WITH TIME TO TERMINATE MANEUVER
 
 TMANUCHK	TC	TIMECHK
 		TC	POSTJUMP

Comanche055/KEYRUPT_UPRUPT.s

@@ -127,7 +127,7 @@ ELRCODE		OCT	22
 # THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
 # THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
 # WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE.
-# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
+# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
 # BY 15 ZEROS.  THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
 # FAILURE).
 #

Comanche055/P20-P25.s

@@ -420,7 +420,7 @@ DE-GR-50	TC	2PHSCHNG
 #
 # ABORT MODES:  P23 ABORT IF MARKING SYSTEM OR EXTENDED VERB ACTIVE
 #
-# INPUT:  NONE REQURIES, NORMALLY CALLED BY P23
+# INPUT:  NONE REQUIRES, NORMALLY CALLED BY P23
 #
 # OUTPUT:  TRUNNION BIAS ANGLE: ANGLE DETERMINED WHEN SHAFT LINE OF SIGHT
 #	(SLOS) AND LANDMARK LINE OF SIGHT (LLOS) ARE SUPERIMPOSED.  THIS ANGLE
@@ -1407,7 +1407,7 @@ INITB		STORE	W +90D,1	# CLEAR 54 - 89
 #
 #		OMETATHSM = (REFSMMAT)(OMEGATH).
 #
-#	(10)	OBTAIN GIMBAL ANGLE INCREMETNS FOR 0.1 SECOND.
+#	(10)	OBTAIN GIMBAL ANGLE INCREMENTS FOR 0.1 SECOND.
 #
 #		DTHETASM = (0.1)(OMEGATHSM)
 #
@@ -1776,7 +1776,7 @@ FURST3		EQUALS	13,14,15	# CONSTANT FOR AUTOCK (OCT 70000).
 # ..... S22.1 ORBITAL NAVIGATION ROUTINE
 # MOD 1
 #
-# FUNCTONAL DESCRIPTION
+# FUNCTIONAL DESCRIPTION
 #	1.  UPDATE CSM STATE VECTOR
 #	2.  UPDATE LANDMARK POSITION
 #	3.  CONVERT W MATRIX FROM 9 TO 6 DIMENSIONS

Comanche055/P32-P33_P72-P73.s

@@ -42,7 +42,7 @@
 # MOD BY WHITE, P.	DATE 1 JUNE 67
 #
 # PURPOSE
-#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WTIH THE FOLLOWING
+#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING
 #		CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
 #		INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
 #		(CDH) MANEUVER.

Comanche055/P34-35_P74-75.s

@@ -31,7 +31,7 @@
 
 
 # Page 460
-# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74)
+# TRANSFER PHASE INITIATION (TPI) PROGRAMS (P34 AND P74)
 # MOD NO -1			LOG SECTION -- P32-P35, P72-P75
 # MOD BY WHITE, P.		DATE: 1 JUNE 67
 #

Comanche055/P37_P70.s

@@ -44,7 +44,7 @@
 # DESCRIPTION
 #	A RETURN TO EARTH TRAJECTORY IS COMPUTED PROVIDED THE CSM IS OUTSIDE THE LUNAR SPHERE OF INFLUENCE AT THE
 #	TIME OF IGNITION.  INITIALLY A CONIC TRAJECTORY IS DETERMINED AND RESULTING IGNITION AND REENTRY PARAMETERS ARE
-# 	DISPLAYED TO THE ASTRONAUT.  THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WTIH THE
+# 	DISPLAYED TO THE ASTRONAUT.  THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WITH THE
 # 	RESULTING IGNITION AND REENTRY PARAMETERS DISPLAYED.  UPON FINAL ACCEPTANCE BY THE ASTRONAUT, THE PROGRAM
 # 	COMPUTES AND STORES THE TARGET PARAMETERS FOR RETURN TO EARTH FOR USE BY SPS PROGRAM (P40) OR RCS PROGRAM (P41).
 #

Comanche055/P51-P53.s

@@ -318,7 +318,7 @@ V06N89*		VN	0689
 # FUNCTION -- TO DISPLAY THE LANDING SITE LATITUDE,
 # LONGITUDE AND ALTITUDE.  TO ACCEPT NEW DATA VIA
 # THE KEYBOARD.  TO COMPUT THE LANDING SITE
-# ORIENTATIION FOR P52 OR P54.
+# ORIENTATION FOR P52 OR P54.
 #
 # LET:
 #	RLS  = LANDING SITE VECTOR IN REF COORDINATES
@@ -1633,7 +1633,7 @@ MKDNCDR		ECADR	MARKDOWN
 # MOD. NO. 2						21 DEC 66
 # MOD. BY STURLAUGSON
 #
-# FUNCTIONAL DESCRIPTIION:
+# FUNCTIONAL DESCRIPTION:
 #
 #	TO PERFORM A SATISFACTORY NUMBER OF SIGHTING MARKS FOR THE REQUESTING PROGRAM (OR ROUTINE).  SIGHTINGS
 # 	CAN BE MADE ON A STAR OR LANDMARK.  WHEN THE CMC ACCEPTS A MARK IT RECORDS AND STORES 5 ANGLES (3 ICDUS AND 2
@@ -1682,7 +1682,7 @@ R53A		CA	MARKINDX	# NUMBER OF MARKS
 		CADR	OPTSTALL
 		TC	CURTAINS
 		INDEX	MARKSTAT
-		CCS	QPRET		# NUMNBER OF MARKS ACTUALLY DONE
+		CCS	QPRET		# NUMBER OF MARKS ACTUALLY DONE
 		TCF	R53B
 		TCF	+2		# ZERO
 		TCF	+1		# CCS HOLE

Comanche055/P61-P67.s

@@ -343,7 +343,7 @@ POSECADR	2CADR	CM/POSE
 # MOD BY:	R. HIRSCHKOP
 # MOD NO: 2	MOD BY: RR BAIRNSFATHER		DATE: 8 MAY 68		REVISED COMMENTS FOR COLOSSUS
 # FUNCTION:	1.  TO START ENTRY GUIDANCE AT .05G SELECTING ROLL ATTITUDE, CONSTANT DRAG LEVEL, AND
-#		    DRAG THRESHHOLD, KA, WHICH ARE KEYED TO THE .05G POINT.
+#		    DRAG THRESHOLD, KA, WHICH ARE KEYED TO THE .05G POINT.
 #		2.  SELECT FINAL PHASE P67 IF V < 27000 FPS WHEN .2G OCCURS.
 #		3.  ITERATE FOR UP-CONTROL SOLUTION P65 IF V > 27000 FPS AND IF ALTITUDE RATE AND DRAG
 #		    LEVEL CONDITIONS ARE SATISFIED.  ENTER P65 WHEN CONSTANT DRAG CONTROLLER HAS BROUGHT RANGE
@@ -950,7 +950,7 @@ DUMPFISH	GOTO
 # MOD NO: 2	MOD BY: RR BAIRNSFATHER		DATE: 21 NOV 67		VARIABLE MU ADDED.
 # MOD NO: 3	MOD BY: RR BAIRNSFATHER		DATE: 21 MAR 68		ACCEPT DIFFERENT EARTH/MOON SCALE
 #
-# FUNCTONAL DESCRIPTION:  EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO
+# FUNCTIONAL DESCRIPTION:  EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO
 #	HORIZONTAL) GIVEN THE SCALAR QUANTITIES:  PRESENT RADIUS AND VELOCITY AND THE TERMINAL RADIUS.
 #	THE USER MUST APPEND PROPER SIGN TO GAMMA, SINCE IT IS CALCULATED AS A POSITIVE NUMBER.
 #	THE EQUATIONS ARE

Comanche055/P76.s

@@ -37,7 +37,7 @@
 #	BEEN TRANSFORMED FROM LV TO REF COSYS).  USING INTEGRVS, THE PROGRAM THEN INTEGRATES THE OTHER
 #	VEHICLE STATE VECTOR TO THE STATE VECTOR OF THIS VEHICLE, THUS INSURING THAT THE W-MATRIX AND BOTH VEHICLE
 #	STATES CORRESPOND TO THE SAME TIME.
-# 3)	ERASABLE INIITIALIZATION REQUIRED -- NONE.
+# 3)	ERASABLE INITIALIZATION REQUIRED -- NONE.
 # 4)	CALLING SEQUENCES AND EXIT MODES -- CALLED BY ASTRONAUT REQUEST THRU DSKY V 37 E 76E.
 #	EXITS BY TCF ENDOFJOB.
 # 5)	OUTPUT -- OTHER VEHICLE STATE VECTOR INTEGRATED TO TIG AND INCREMENTED BY DELTA V IN REF COSYS.

Comanche055/PHASE_TABLE_MAINTENANCE.s

@@ -99,7 +99,7 @@ DSPMMJOB	EQUALS	DSPMMJB
 # WHERE EACH LETTER OR NUMBER STANTS FOR A BIT.  THE G'S STAND FOR THE GROUP, OCTAL 1-7, THE P'S FOR THE PHASE,
 # OCTAL 0 - 127.  0'S MUST BE 0.  IF ONE WISHES TO HAVE THE TBASE OF GROUP G TO BE SET AT THIS TIME,
 # T IS SET TO 1, OTHERWISE IT IS SET TO 0.  SIMILARLY IF ONE WISHES TO SET LONGBASE, THEN L IS SET TO 1, OTHERWISE
-# IT IS SET TO 0.  SOME EXAMLES,
+# IT IS SET TO 0.  SOME EXAMPLES,
 #		TC	PHASCHNG	# THIS WILL CAUSE GROUP 3 TO BE SET TO 0,
 #		OCT	00003		# MAKING GROUP 3 INACTIVE
 #

Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s

@@ -84,7 +84,7 @@
 # Page 308
 #		2)	EXTENDED VERBS TO TO THE EXTENDED VERB FAN AS PART OF THE
 #			PINBALL EXECUTIVE JOB WITH PRIORITY 30000.  IT IS THE 
-#			RESPONSIBILITY OF THE EXTEDED VERB CALLED TO EVENTUALLY
+#			RESPONSIBILITY OF THE EXTENDED VERB CALLED TO EVENTUALLY
 #			CHANGE PRIORITY (IF NECESSARY) AD DO AN ENDOFJOB.
 #			ALSO PINBALL IS A NOVAC JOB.  EBANK SET FOR COMMON.
 #		3)	VERB 37.  CHANGE OF PROGRAM (MAJOR MODE) CALLS `V37' IN THE
@@ -1128,7 +1128,7 @@ GODSPALM	TC	POSTJUMP
 # S'S ARE THE SF ROUTINE 1 CODE NUMBER
 #
 # IN OCTAL DISPLAY AND LOAD (OCT OR DEC) VERBS, EXCLUDE USE OF VERBS WHOSE
-# COMPONENT NUMBER IS GREATER THAN THE NUMBER OF COMONENTS IN NOUN.
+# COMPONENT NUMBER IS GREATER THAN THE NUMBER OF COMPONENTS IN NOUN.
 # (ALL MACHINE ADDRESS TO BE SPECIFIED NOUNS ARE 3 COMPONENT.)
 #
 # IN MULTI-COMPONENT LOAD VERBS, NO MIXING OF OCTAL AND DECIMAL DATA
@@ -2817,7 +2817,7 @@ SETVAC		CAF	TCFINDVC
 		
 # VBRQWAIT ENTERS REQUEST TO WAITLIST FOR ANY ADDRESS WITH ANY DELAY.
 # IT DOES ENDOFJOB AFTER ENTERING REQUEST.  DISPLAY SYST IS RELEASED.
-# IT ASSUMES NOUN 26 HAS BEEN PRELOADED WTIH
+# IT ASSUMES NOUN 26 HAS BEEN PRELOADED WITH
 #	COMPONENT 1	DELAY (LOW BITS)
 #	COMPONENT 2	TASK ADRES (12 BIT)
 #	COMPONENT 3	BBCON
@@ -2921,11 +2921,11 @@ ENDRELDS	EQUALS
 # PLACE 0VVVVVVVNNNNNNN INTO A.
 # V'S ARE THE 7-BIT VERB CODE.  N'S ARE THE 7-BIT NOUN CODE.
 #
-# IF NVSUB IS CALLED WTIH THE FOLLOWING NEGATIVE NUMBERS (RATHER THAN THE
+# IF NVSUB IS CALLED WITH THE FOLLOWING NEGATIVE NUMBERS (RATHER THAN THE
 # VERB-NOUN CODE) IN A, THEN THE DISPLAY IS BLANKED AS FOLLOWS ---
 # -4 FULL BLANK, -3 LEAVE MODE, -2 LEAVE MODE AND VERB, -1 BLANK R'S ONLY.
 #
-# NVSUB CAN BE USED WTIH MACHINE CADR TO BE SPECIFIED BY PLACING THE CADR INTO
+# NVSUB CAN BE USED WITH MACHINE CADR TO BE SPECIFIED BY PLACING THE CADR INTO
 # MPAC+2 BEFORE THE STANDARD NVSUB CALL.
 #
 # NVSUB RETURNS TO 2+ CALLING LOC AFTER PERFORMING TASK, IF DISPLAY
@@ -2942,7 +2942,7 @@ ENDRELDS	EQUALS
 # THE DISPLAY SYSTEM IS BLOCKED BY THE DEPRESSION OF ANY
 # KEY, EXCEPT ERROR LIGHT RESET.
 # IT IS RELEASED BY THE KEY RELEASE BUTTON, ALL EXTENDED VERBS,
-# PROCED WITOHOUT DATA, TERMINATE, RESEQUENCE, INITIALIZE EXECUTIVE,
+# PROCEED WITHOUT DATA, TERMINATE, RESEQUENCE, INITIALIZE EXECUTIVE,
 # RECALL PART OF RECALTST IF ENDIDLE WAS USED,
 # VB = REQUEST EXECUTIVE, VB = REQUEST WAITLIST,
 # MONITOR SET UP.
@@ -2960,7 +2960,7 @@ ENDRELDS	EQUALS
 # (SIMILARLY FOR PLEASE MARK).  FIRST PLACE THE CODED NUMBER FOR WHAT
 # ACTION IS DESIRED OF OPERATOR INTO THEREGISTERS REFERRED TO BY THE
 # `CHECKLIST' NOUN.  GO TO NVSUB WITH A DISPLAY VERB AND THE `CHECKLIST'
-# NOUN.  GO TO NVSUB AGAIN WTIH THE `PLEASE PERFORM' VERB AND ZEROS IN THE
+# NOUN.  GO TO NVSUB AGAIN WITH THE `PLEASE PERFORM' VERB AND ZEROS IN THE
 # LOW 7 BITS.  THIS `PASTES UP' THE `PLEASE PERFORM' VERB INTO THE VERB
 # LIGHTS.
 #

Comanche055/PINBALL_NOUN_TABLES.s

@@ -120,7 +120,7 @@
 # (WHICH ARE IN A SEPARATE BANK FROM THE REST OF PINBALL).  THESE READING
 # ROUTINES ARE IN THE SAME BANK AS THE TABLES.  THEY ARE CALLED BY DXCH Z.
 
-# LODNNTAB LOADS NNADTEM WTIH THE NNADTAB ENTRY, NNTYPTEM WITH THE
+# LODNNTAB LOADS NNADTEM WITH THE NNADTAB ENTRY, NNTYPTEM WITH THE
 # NNTYPTAB ENTRY.  IF THE NOUN IS MIXED, IDADITEM IS LOADED WITH THE FIRST
 # IDADDTAB ENTRY, IDAD2TEM THE SECOND IDADDTAB ENTRY, IDAD3TEM THE THIRD
 # IDADDTAB ENTRY, RUTMXTEM WITH THE RUTMXTAB ENTRY.  MIXBR IS SET FOR
@@ -165,7 +165,7 @@ LODNLV		DXCH	IDAD2TEM		# PUT RETURN INFO INTO A, L.
 		
 MIXCON		=	OCT50			# FIRST MIXED NOUN =40.  (DEC 40)
 
-# GTSFOUT LOADS SFTEMP1, SFTEMP2 WTIH THE DP SFOUTAB ENTRIES.
+# GTSFOUT LOADS SFTEMP1, SFTEMP2 WITH THE DP SFOUTAB ENTRIES.
 # Page 271
 
 GTSFOUT		DXCH	SFTEMP1			# 2X (SFCONUM) ARRIVES IN SFTEMP1.
@@ -214,7 +214,7 @@ NNADTAB		OCT	00000			# 00 	NOT IN USE
 		OCT	00000			# 23	SPARE
 		ECADR	DSPTEM2 +1		# 24	DELTA TIME FOR AGC CLOCK (HRS,MIN,SEC)
 		ECADR	DSPTEM1			# 25	CHECKLIST
-						#	(USED WTIH PLEASE PERFORM ONLY)
+						#	(USED WITH PLEASE PERFORM ONLY)
 		ECADR	DSPTEM1			# 26	PRIO/DELAY, ADRES, BBCON
 		ECADR	SMODE			# 27	SELF TEST ON/OFF SWITCH
 # Page 272
@@ -588,7 +588,7 @@ SFOUTAB		OCT	05174			# WHOLE, DP TIME (SEC)
 		OCT	15340
 		OCT	01031			# VELOCITY3	(POINT BETWN BITS 7-8)
 		OCT	21032
-		OCT	34631			# ELEVATION DETREES
+		OCT	34631			# ELEVATION DEGREES
 		OCT	23146
 		OCT	14340			# TRIM DEGREES
 		OCT	24145

Comanche055/R60_62.s

@@ -159,7 +159,7 @@ V06N18		VN	0618
 # BEGINNING WITH THE LOCATION CALLED SCAXIS.  THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
 # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
 # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM.  THE COMPONENTS OF THIS
-# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES.  WITH THIS INFORMTION VECPOINT COMPUTES A SET OF THREE GIMBAL
+# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES.  WITH THIS INFORMATION VECPOINT COMPUTES A SET OF THREE GIMBAL
 # ANGLES (2'S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
 # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
 #

Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s

@@ -295,7 +295,7 @@ TENTHSEK	TS	ATTSEC
 #	    ALSO IGNORE AUTOMATIC STEERING
 #	    SET = + BY
 #		1) INITIALIZATION PHASE OF AUTOPILOT
-#		2) OCCURANCE OF RHC COMMANDS
+#		2) OCCURRENCE OF RHC COMMANDS
 #		3) FREE MODE
 #		4) SWITCH OVER TO ATTITUDE HOLD FROM AUTO
 #		   WHILE DOING AUTOMATIC STEERING (IN THIS CASE

Comanche055/RT8_OP_CODES.s

@@ -136,7 +136,7 @@ TPMODE		CAF	ONE		# MODE IS TP.
 # Page 1510
 		TC	Q
 
-		INDEX	A		# OVERFLOW UNCORRECT AND IN MSU.
+		INDEX	A		# OVERFLOW INCORRECT AND IN MSU.
 		CAF	LIMITS
 		ADS	MPAC
 		TC	Q

Comanche055/STABLE_ORBIT.s

@@ -86,7 +86,7 @@
 #	(6)  DELVTPI	MAGNITUDE OF DELTA V AT SOI (SOR) TIME
 #	(7)  DELVTPF	MAGNITUDE OF DELTA V AT INTERCEPT TIME
 #	(8)  DELTA 	VELOCITY AT SOI (AND SOR) - LOCAL VERTICAL
-#			CORDINATES
+#			COORDINATES
 #
 # SUBROUTINES USED
 #

Comanche055/SXTMARK.s

@@ -520,7 +520,7 @@ REJECT3		CAF	LOW9			# DECREMENT POINTER TO REJECT MARK
 		TC	RESUME
 		
 # Page 232
-# PROGRAM DESCRIPTON MKVB51 AND MKVB50
+# PROGRAM DESCRIPTION MKVB51 AND MKVB50
 #
 # AUTHOR: 	BARNERT		DATE: 2-15-67		MOD: 0
 # PURPOSE:	FLASH V51N70,V51N43, OR V51 TO REQUEST MARKING,

Comanche055/T4RUPT_PROGRAM.s

@@ -577,7 +577,7 @@ NXTFL33		CCS	RUPTREG2		# PROCESS POSSIBLE ADDITIONAL CHANGES.
 #
 # ERASABLE INITIALIZATION:
 #		1) FRESH START OR RESTART WITH NO GROUPS ACTIVE:  C(CDUZ) = 0, IMODES30 BIT 6 = 0, IMODES33 BIT 1 = 0.
-#		2) RESTART WTIH GROUPS ACTIVE:	SAME AS FRESH START EXCEPT C(CDUZ) NOT CHANGED SO GIMBAL MONITOR
+#		2) RESTART WITH GROUPS ACTIVE:	SAME AS FRESH START EXCEPT C(CDUZ) NOT CHANGED SO GIMBAL MONITOR
 #						PROCEEDS AS BEFORE.
 #
 # ALARMS:	1) MGA REGION (2) CAUSES GIMBAL LOCK LAMP TO BE LIT.
@@ -863,7 +863,7 @@ IMUOP2		CAF	BIT2			# SEE IF FAILED ISS TURN-ON SEQ IN PROG.
 #
 # JOBS OR TASKS INITIATED:  NONE.
 #
-# SUBROUTINES CALLED:  1) SETISSW, AND 2) ALARM (SEE FUNCITONAL DESCRIPTION).
+# SUBROUTINES CALLED:  1) SETISSW, AND 2) ALARM (SEE FUNCTIONAL DESCRIPTION).
 #
 # ERASABLE INITIALIZATION:  SEE IMUMON FOR INITIALIZATION OF IMODES30.  THE RELEVANT BITS ARE 5, 7, 8, 9, AND 10.
 #

Comanche055/TIME_OF_FREE_FALL.s

@@ -31,7 +31,7 @@
 # Page 1373
 # THE TFF SUBROUTINES MAY BE USED IN EITHER EARTH OR MOON CENTERED COORDINATES.  THE TFF ROUTINES NEVER
 # KNOW WHICH ORIGIN APPLIES.  IT IS THE USER WHO KNOWS, AND WHO SUPPLIES RONE, VONE, AND 1/SQRT(MU) AT THE
-# APPROPIRATE SCALE LEVEL FOR THE PROPER PRIMARY BODY.
+# APPROPRIATE SCALE LEVEL FOR THE PROPER PRIMARY BODY.
 #
 #	EARTH ORIGIN	POSITION	-29	METERS
 #			VELOCITY	-7	METERS/CENTISECOND
@@ -81,7 +81,7 @@ NRMAG		=	32D	#	PRESENT RADIUS  M	E: (-29+NR)
 TFFX		=	34D     #
 TFFTEM		=	36D	#	TEMPORARY
 # Page 1374
-#		REGISTERS S1, S2 ARE UNTOUCED BY ANY TFF SUBROUTINE
+#		REGISTERS S1, S2 ARE UNTOUCHED BY ANY TFF SUBROUTINE
 #		INDEX REGISTERS X1, X2 ARE USED BY ALL TFF SUBROUTINES.  THEY ARE ESTAB-
 #		LISHED IN TFF/CONIC AND MUST BE PRESERVED BETWEEN CALLS TO SUBSEQUENT
 #		SUBROUTINES.
@@ -341,7 +341,7 @@ DUMPRPRA	RVQ
 #		             2      3             2
 #		1/3 - X/5 + X /7 - X /8 ...	(X  < 1.0)
 #
-# CALLING SEQUENC:	TIME TO RTERM			TIME TO PERIGEE
+# CALLING SEQUENCE:	TIME TO RTERM			TIME TO PERIGEE
 #			CALL				CALL
 #				CALCTFF				CALCTPER
 #			C(MPAC) = TERMNL RAD M		C(MPAC) = PERIGEE RAD M

Comanche055/TVCEXECUTIVE.s

@@ -100,7 +100,7 @@ ROLLPREP	CAE	CDUX		# UPDATE ROLL LADDERS (NO NEED TO RESTART-
 		XCH	OGANOW		# 	PROTECT, SINCE ROLL DAPS RE-START)
 		XCH	OGAPAST
 		
-		CAE	OGAD		# PREPARE ROLL FDAI NEEDLE WTIH FLY-TO
+		CAE	OGAD		# PREPARE ROLL FDAI NEEDLE WITH FLY-TO
 		EXTEND			#	ERROR (COMMAND - MEASURED)
 		MSU	OGANOW
 		TS	AK		# FLY-TO OGA ERROR, SC.AT B-1 REVS

Comanche055/TVCRESTARTS.s

@@ -122,7 +122,7 @@
 #
 # OTHER INTERFACES....DOTVCON AND RCSDAPON (T5 BITS), ELRSKIP (CALLS IT)
 #
-# ERASABLE ININTIALIZATION REQUIRED....
+# ERASABLE INITIALIZATION REQUIRED....
 #
 #      *T5 BITS (1,0), TVCPHASE (-2,-1,0,1,2,3), TVCEXPHS (1 THRU 6)
 #      *TVC DAP VARIABLES

Comanche055/TVCSTROKETEST.s

@@ -41,8 +41,8 @@
 #		IMMEDIATELY.  IF NOT CSM/LM, PROGRAM EXITS WITH NO ACTION.
 #	HACK (STROKE TEST) GENERATES THE WAVEFORM BY DUMPING PULSE BURSTS
 #		OF PROPER SIGN AND IN PROPER SEQUENCE DIRECTLY INTO
-#		TVCPITCH, WORKING IN CONJUNCITON WITH BOTH PITCH AND YAW
-#		TVC DAPS, WITH INTERMEDIAT WAITLIST CALLS.  NOTE, HOWEVER
+#		TVCPITCH, WORKING IN CONJUNCTION WITH BOTH PITCH AND YAW
+#		TVC DAPS, WITH INTERMEDIATE WAITLIST CALLS.  NOTE, HOWEVER
 #		THAT THE STROKE TEST IS PERFORMED ONLY IN THE PITCH AXIS.
 #		AN EXAMPLE WAVEFORM IS GIVEN BELOW, TO DEMONSTRATE STROKE-
 #		TEST PARAMETER SELECTION.

Comanche055/UPDATE_PROGRAM.s

@@ -122,7 +122,7 @@
 #		V33E		VERB 33 TO SIGNAL THAT THE STATE VECTOR IS READY TO BE STORED.
 #
 #	2.  REFSMMAT (ALL DATA ENTRIES IN OCTAL)
-#		ENTRIES		DATA DEFINITITIONS				SCALE FACTORS:
+#		ENTRIES		DATA DEFINITIONS				SCALE FACTORS:
 # Page 1499
 #		V71E		CONTIGUOUS BLOCK UPDATE VERB
 #		   24E		NUMBER OF COMPONENTS FOR REFSMMAT UPDATE

Luminary099/AOTMARK.s

@@ -243,7 +243,7 @@ OANB		SETPD	STQ
 		GOTO
 			GCTR
 # Page 250
-# SURFSTAR COMPUTES A STAR VECTOR IN SM COORDINAGES FOR LUNAR
+# SURFSTAR COMPUTES A STAR VECTOR IN SM COORDINATES FOR LUNAR
 # SURFACE ALIGNMENT AND EXITS TO AVEIT TO AVERAGE STAR VECTORS.
 # 
 #	GIVEN	X-MARK PLANE 1/4 VEC IN NB AT 18D OF LOCAL VAC

Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s

@@ -890,7 +890,7 @@ REP40ALM	CAF	V05N09		# (14)
 		TCF	+2		# PROCEED 	CHECK FOR P42
 		TCF	REP40ALM	# V32E		REDISPLAY ALARM
 
-		INDEX	WHICH		# FOR P42, ALLOW CREW TO PRECEED EVEN
+		INDEX	WHICH		# FOR P42, ALLOW CREW TO PROCEED EVEN
 		TCF	14		# THOUGH VEHICLE IS UNSTAGED.
 
 #	********************************

Luminary099/DOWN_TELEMETRY_PROGRAM.s

@@ -115,7 +115,7 @@
 #		SAME AS ECADR, BUT USED WHEN THE WORD ADDRESSED IS THE LEFT
 #		HALF OF A DOUBLE-PRECISION WORD FOR DOWN TELEMETRY.
 #	B.	2DNADR - 6DNADR		N-WORD DOWNLIST ADDRESS, N = 2 - 6.
-#		SAME AS 1DNADR, BUT WTIH THE 4 UNUSED BITS OF THE ECADR FORMAT
+#		SAME AS 1DNADR, BUT WITH THE 4 UNUSED BITS OF THE ECADR FORMAT
 #		FILLED IN WITH 0001-0101.  USED TO POINT TO A LIST OF N DOUBLE-
 #		PRECISION WORDS, STORED CONSECUTIVELY, FOR DOWN TELEMETRY.
 #	C.	DNCHAN			DOWNLIST CHANNEL ADDRESS.
@@ -339,7 +339,7 @@ SUBLIST		EQUALS 	DNQ
 #	AFTER KEYING IN V74E THE CURRENT DOWNLIST WILL BE IMMEDIATELY TERMINATED AND THE DOWNLINK ERASABLE DUMP
 #	WILL BEGIN.
 #
-#	ONCE INITITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
+#	ONCE INITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
 #	BY THE FOLLOWING:
 #
 #	1.	A FRESH START

Luminary099/FINDCDUW--GUIDAP_INTERFACE.s

@@ -289,7 +289,7 @@ DELGMBLP	TS	TEM2
 		TS	CPHI		# OUTPUTS TO NOUN22
 		EXTEND
 		INDEX	TEM2
-		MSU	CDUXD		# NO MATTER THAT THESE SLIGHLTY DIFFERENT
+		MSU	CDUXD		# NO MATTER THAT THESE SLIGHTLY DIFFERENT
 		COM			# FROM WHEN WE INITIALLY FETCHED THEM
 		INDEX	TEM2
 		TS	-DELGMB		# -UNLIMITED GIMBAL ANGLE CHGS, 1'S, PI

Luminary099/IMU_PERFORMANCE_TESTS_4.s

@@ -32,7 +32,7 @@
 # BY --		GEORGE SCHMIDT IL7-146 EXT 1126
 # MOD NO-ZERO
 #
-# FUNCITONAL DESCRIPTION
+# FUNCTIONAL DESCRIPTION
 #
 # THIS SECTION CONSISTS OF THE FILTER FOR THE GYRO DRIFT TESTS.  NO COMPASS
 # IS DONE IN LEM.  FOR A DESCRIPTION OF THE FILTER SEE E-1973.  THIS

Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s

@@ -415,7 +415,7 @@ REDES1		DLOAD	DSU
 #	VELOCITY RELATIVE TO THE SURFACE
 #		_______   _   _   __
 #		ANGTERM = V + R * WM
-#	STATE IN GUIDANCE COORDINTES:
+#	STATE IN GUIDANCE COORDINATES:
 #		___   *   _   ____
 #		RGU = CG (R - LAND)
 #		___   *   _   __   _
@@ -1257,11 +1257,11 @@ DESCBITS	MASK	BIT7		# COME HERE FROM MARKRUPT CODING WITH BIT
 #
 # PRECAUTION:  ROOTPSRS MAKES NO CHECKS FOR OVERFLOW OR FOR IMPROPER USAGE.  IMPROPER USAGE COULD
 # PRECLUDE CONVERGENCE OR REQUIRE EXCESSIVE ITERATIONS.  AS A SPECIFIC EXAMPLE, ROOTPSRS FORMS A DERIVATIVE
-# COEFFICIENT TABLE BY MULTIPLYINE EACH A(I) BY I, WHERE I RANGES FROM 1 TO N.  IF AN ELEMENT OF THE DERIVATIVE
-# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED.  ROOTPSRS MAY CONVERGE ON THE COREECT
+# COEFFICIENT TABLE BY MULTIPLYING EACH A(I) BY I, WHERE I RANGES FROM 1 TO N.  IF AN ELEMENT OF THE DERIVATIVE
+# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED.  ROOTPSRS MAY CONVERGE ON THE CORRECT
 # ROOT NONETHELESS, BUT IT MAY TAKE AN EXCESSIVE NUMBER OF ITERATIONS.  THEREFORE THE USER SHOULD RECOGNIZE:
 #	1.  USER'S RESPONSIBILITY TO ASSUR THAT I X A(I) < 1 IN MAGNITUDE FOR ALL I.
-#	2.  USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUTATING EITHER THE RESIDUAL OR THE DERIVATIVE
+#	2.  USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUATING EITHER THE RESIDUAL OR THE DERIVATIVE
 #	    POWER SERIES.  THIS OVERFLOW WOULD BE PRODUCED BY SUBROUTINE POWRSERS, CALLED BY ROOTPSRS, AND MIGHT NOT
 #	    PRECLUDE EVENTUAL CONVERGENCE.
 #	3.  AT PRESENT, ERASABLE LOCATIONS ARE RESERVED ONLY FOR N UP TO 5.  AN N IN EXCESS OF 5 WILL PRODUCE CHAOS.

Luminary099/P-AXIS_RCS_AUTOPILOT.s

@@ -964,7 +964,7 @@ HEADTJET	CA	ZERO
 -FOURDEG	DEC	-.08888
 
 # Page 1440
-# JET POLICY CONTSTRUCTION SUBROUTINE
+# JET POLICY CONSTRUCTION SUBROUTINE
 #
 # INPUT:	ROTINDEX, NUMBERT
 #

Luminary099/P30_P37.s

@@ -90,7 +90,7 @@ V06N33		VN	0633
 V06N42		VN	0642
 
 # Page 616
-# PROGRAM DESCRPTION S30.1	DATE 9NOV66
+# PROGRAM DESCRIPTION S30.1	DATE 9NOV66
 # MOD NO 1			LOG SECTION P30,P37
 # MOD BY RAMA AIYAWAR **
 #

Luminary099/P32-P35_P72-P75.s

@@ -34,7 +34,7 @@
 #
 # PURPOSE
 
-#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WTIH THE TIME FOLLOWING
+#	(1)	TO CALCULATE PARAMETERS ASSOCIATED WITH THE TIME FOLLOWING
 #		CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
 #		INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
 #		(CDH) MANEUVER.

Luminary099/P70-P71.s

@@ -236,7 +236,7 @@ GOABORT		TC	INTPRET
 		TC	DOWNFLAG
 		ADRES	IDLEFLAG
 		
-		TC	UPFLAG		# INSURE 4-JET TRANSLATION CAPABILIITY.
+		TC	UPFLAG		# INSURE 4-JET TRANSLATION CAPABILITY.
 		ADRES	ACC4-2FL
 		
 		TC	CHECKMM

Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s

@@ -476,7 +476,7 @@ QERRCALC	CAE	CDUY		# Q-ERROR CALCULATION
 		TS	DAPTEMP2	# SAVE FOR RERRCALC
 		EXTEND
 		MP	M22		# (CDUZ-CDUZD)*M22 SCALED AT PI RADIANS
-		AD	DELQEROR	# KALCMANU INERFACE ERROR
+		AD	DELQEROR	# KALCMANU INTERFACE ERROR
 		AD	E
 		XCH	QERROR		# SAVE Q-ERROR FOR EIGHT-BALL DISPLAY.
 
@@ -487,7 +487,7 @@ RERRCALC	CAE	DAPTEMP1	# R-ERROR CALCULATION:
 		CAE	DAPTEMP2	# SECOND TERM CALCULATION:
 		EXTEND			# CDU ANGLE -ANGLE DESIRED (Z-AXIS)
 		MP	M32		# (CDUZ-CDUZD)*M32 SCALED AT PI RADIANS
-		AD	DELREROR	# KALCMANU INERFACE ERROR
+		AD	DELREROR	# KALCMANU INTERFACE ERROR
 		AD	E
 		XCH	RERROR		# SAVE R-ERROR FOR EIGHT-BALL DISPLAY.
 		TC	Q
@@ -538,7 +538,7 @@ TJLAW		CA	TJLAWADR
 		CADR	SPSRCS		# DETERMINE RCS CONTROL
 		RELINT
 		CAF	FOUR		# ALWAYS CALL FOR 2-JET CONTROL ABOUT U,V.
-		TS	NUMBERT		# FALL THROUGH TO JET SLECTION, ETC.
+		TS	NUMBERT		# FALL THROUGH TO JET SELECTION, ETC.
 
 # Q,R-JET-SELECTION-LOGIC
 #

Luminary099/RTB_OP_CODES.s

@@ -113,7 +113,7 @@ TPMODE		CAF	ONE		# MODE IS TP.
 		TS	MPAC		# AND SKIP ON OVERFLOW.
 		TC	Q
 
-		INDEX	A		# OVERFLOW UNCORRECT AND IN MSU.
+		INDEX	A		# OVERFLOW INCORRECT AND IN MSU.
 		CAF	LIMITS
 		ADS	MPAC
 		TC	Q

Luminary099/SERVICER.s

@@ -1067,7 +1067,7 @@ MUNRVG		VLOAD	VXSC
 			R1S
 		VXV	VSL2
 			WM
-		STODL	DELVS		# LUNAR ROTATION CORRECTON TERM*2(5) M/CS.
+		STODL	DELVS		# LUNAR ROTATION CORRECTION TERM*2(5) M/CS.
 			36D
 		DSU
 			/LAND/

Luminary099/THE_LUNAR_LANDING.s

@@ -126,7 +126,7 @@ IGNALOOP	DLOAD
 #                                                10
 #                                               2   (VGU - 16 VGU KIGNX/B4)
 #                                                       2        0
-# Page 787 new page is actually one line earlier but this would put the indices on a seperate line 
+# Page 787 new page is actually one line earlier but this would put the indices on a separate line 
 # disconnected from their respective variables
 # THE NUMERATOR IS SCALED IN METERS AT 2(28).  THE DENOMINATOR IS A VELOCITY IN UNITS OF 2(10) M/CS.
 # THE QUOTIENT IS THUS A TIME IN UNITS OF 2(18) CENTISECONDS.  THE FINAL SHIFT RESCALES TO UNITS OF 2(28) CS.

Luminary099/THROTTLE_CONTROL_ROUTINES.s

@@ -131,7 +131,7 @@ DOIT		CA	PIF
 		CA	TIME1
 		TS	TTHROT
 
-# SINCE /AF/ IS NOT AN INSTANTANEOUS ACELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
+# SINCE /AF/ IS NOT AN INSTANTANEOUS ACCELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
 # THE PRECEEDING PIPA INTERVAL, AND SINCE FP IS COMPUTED DIRECTLY FROM /AF/, FP IN ORDER TO CORRESPOND TO THE
 # ACTUAL THRUST LEVEL AT THE END OF THE INTERVAL MUST BE WEIGHTED BY
 #

Luminary099/TJET_LAW.s

@@ -31,7 +31,7 @@
 # Page 1460
 # PROGRAM DESCRIPTION
 # DESIGNED BY:	R. D. GOSS AND P. S. WEISSMAN
-# CODED BY:  P. S. WEISSMAN, 28 FEBRURARY 1968
+# CODED BY:  P. S. WEISSMAN, 28 FEBRUARY 1968
 #
 # TJETLAW IS CALLED AS A SUBROUTINE WHEN THE LEM IS NOT DOCKED AND THE AUTOPILOT IS IN THE AUTOMATIC OR
 # ATTITUDE-HOLD MODE TO CALCULATE THE JET-FIRING-TIME (TJET) REQUIRED FOR THE AXIS INDICATED BY AXISCTR:

Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s

@@ -603,7 +603,7 @@ GMBLBITB	OCTAL	06000		# INDEXED WRT GMBLBITA	DO NOT MOVE *******
 
 # SUBROUTINE ROOTCYCL:	BY CRAIG WORK, 3 APRIL 68
 #
-# ROOTCYCL IS A SUBROUTINE WHICH EXECUTS ONE NEWTON SQUARE ALGORITHM ITERATION.  THE INITIAL GUESS AT THE
+# ROOTCYCL IS A SUBROUTINE WHICH EXECUTES ONE NEWTON SQUARE ALGORITHM ITERATION.  THE INITIAL GUESS AT THE
 # SQUARE ROOT IS PRESUMED TO BE IN THE A REGISTER AND ONE-HALF THE SQUARE IS TAKEN FROM HALFARG.  THE NEW APPROXIMATION
 # TO THE SQUARE ROOT IS RETURNED IN THE A REGISTER.  DEBRIS:  A, L, SR, SCRATCH.  ROOTCYCL IS CALLED FROM
 # LOCATION (LOC) BY A TC ROOTCYCL, AND RETURNS (TC Q) TO LOC +1.